The baseline trajectory for the Cassini mission to Saturn is an Oct. 1997 VVEJGA (Venus-Venus-Earth-Jupiter-Gravity-Assist) trajectory. The current choice for an arrival date, June 25, 2004, provides a rare Phoebe flyby opportunity. The goal of this analysis is to determine the optimal feasible trajectory for any launch/arrival date combination.


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    Title :

    Cassini 1997 VVEJGA Trajectory Launch/Arrival Space Analysis


    Contributors:
    Peralta, F. (author) / Flanagan, S. (author)

    Publication date :

    1993-08-16


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Cassini 1997 VVEJGA Trajectory Launch/Arrival Space Analysis

    Flanagan, S. / Peralta, F. / American Astronautical Society et al. | British Library Conference Proceedings | 1993


    Cassini 1997 VVEJGA Trajectory Launch/Arrival Space Analysis (AAS 93-684)

    Flanagan, S. / Peralta, F. / American Astronautical Society | British Library Conference Proceedings | 1993



    Cassini Launch Contingency Effort

    Chang, Y. / O Neil, J. M. / McGrath, B. E. et al. | British Library Conference Proceedings | 2002


    Cassini Interplanetary Trajectory Design

    Peralta, Fernando / Flanagan, Steve | NTRS | 1995